Abstract
This paper presented discharge coefficients of the expanded holes at inlet and outlet with plane angles of 20°, 45°, 90°, radial angles of 0°, 30°, 65° and the ratios of pitch to diameter of 2, 3, 4. The momentum flux ratios varied in the range from 1 to 8. The results show that discharge coefficients of radial angle =0° increase significantly when the plane angles increase from 20° to 90°. The effect of plane angle becomes weak with the increasing radial angles. Radial angles have weak influence on the discharge coefficients of plane angle=20° and discharges coefficients of plane angle=45° and plane angle=90° decreases when the radial angles increase from 0° to 65°. Discharge coefficients of plane angle=90° increase when the ratios of hole pitch to the diameter increase from 2 to 4.
Original language | English |
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Pages (from-to) | 499-506 |
Number of pages | 8 |
Journal | Hangkong Dongli Xuebao/Journal of Aerospace Power |
Volume | 24 |
Issue number | 3 |
State | Published - Mar 2009 |
Keywords
- Discharge coefficient
- Experiment
- Film cooling
- Turbine